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Flexible Rotor Balancing of a High-Speed Gas Turbine Engine Mechanical Technology Incorporated

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Rieger, N. F. (Neville F.), author.
Conference Name:
National Farm, Construction, Industrial Machinery, Powerplant Meeting (1972-09-11 : Milwaukee, Wisconsin, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1972
Summary:
The need for balancing a high-speed rotor in a manner that accounts for its speed-dependent deformations is discussed. The influence coefficient method of flexible rotor balancing is described with reference to the balancing of an advanced gas turbine engine rotor. This engine rotor-bearing system is then studied in detail as an application of flexible rotor balancing, using the influence coefficient method. The relative effectiveness of various combinations of balance speeds and numbers of balance planes is compared
Notes:
Vendor supplied data
Publisher Number:
720741
Access Restriction:
Restricted for use by site license

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